US11592026B2 - Fan aspirator - Google Patents
Fan aspirator Download PDFInfo
- Publication number
- US11592026B2 US11592026B2 US17/237,304 US202117237304A US11592026B2 US 11592026 B2 US11592026 B2 US 11592026B2 US 202117237304 A US202117237304 A US 202117237304A US 11592026 B2 US11592026 B2 US 11592026B2
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- US
- United States
- Prior art keywords
- fan
- pinion gear
- gear
- aspirator
- motors
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000000034 method Methods 0.000 abstract description 11
- 239000012530 fluid Substances 0.000 abstract description 3
- 230000008901 benefit Effects 0.000 description 8
- 230000004044 response Effects 0.000 description 5
- 230000008569 process Effects 0.000 description 3
- 238000005188 flotation Methods 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 230000001965 increasing effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000000284 resting effect Effects 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 239000003990 capacitor Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 230000015654 memory Effects 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
- F04D25/0606—Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/14—Inflatable escape chutes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/16—Dinghy stowage
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/002—Axial flow fans
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
- F04D25/0606—Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
- F04D25/066—Linear Motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/08—Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
Definitions
- the present disclosure is directed to aircraft evacuation systems, and more particularly to a fan aspirator for inflating flotation devices and inflation assemblies for evacuation systems.
- Conventional evacuation systems of aircraft generally include an inflatable device, such as an evacuation slide, an aspirator for inflating the inflatable device, and a source of compressed gas (e.g., one or more tank of compressed gas).
- a source of compressed gas e.g., one or more tank of compressed gas
- the source of compressed gas may release gas through the aspirator, which then also draws air from the environment of the aspirator and inflates the inflatable device using the decompressed gas and the air.
- compressed gas storage tanks may be undesirable for various reasons. For example, the storage tanks may undesirably increase a total weight of the aircraft. Additionally, the storage tanks may be difficult to store and transport on board the aircraft.
- the present disclosure provides a fan aspirator that includes a housing, a fan, a pinion gear, and at least one motor.
- the housing defines a central channel and has a central longitudinal axis, according to various embodiments.
- the fan is disposed in the central channel and is configured to rotate about a rotational axis that is substantially parallel to the central longitudinal axis, according to various embodiments.
- the pinion gear may be coupled to the fan and may be configured to rotate with the fan, with the pinion gear comprising an annular body with a gear track.
- the at least one motor comprises a drive gear, with the motor being coupled to the housing and the drive gear being mechanically coupled to the gear track of the annular body of the pinion gear, wherein the fan is configured to be driven via the drive gear and the pinion gear.
- the motor is a first motor of a plurality of motors having a respective plurality of drive gears.
- the plurality of motors may be coupled to the housing and may be distributed circumferentially around the rotational axis such that each drive gear of the respective plurality of drive gears is mechanically coupled to the gear track of the annular body of the pinion gear.
- the plurality of motors comprises at least 4 motors. In various embodiments, the plurality of motors comprises at least 6 motors.
- the gear track is disposed on a radially outward surface of the annular body of the pinion gear such that the plurality of motors are circumferentially distributed around a periphery of the pinion gear.
- a radially inward surface of the annular body of the pinion gear is radially outward of tips of fan blades of the fan such that a radial gap is defined between the tips of the fan blades and the radially inward surface of the annular body of the pinion gear.
- a radially inward surface of the central channel of the housing at an axial location of fan blades of the fan is radially outward of tips of the fan blades such that a radial gap is defined between the tips of the fan blades and the radially inward surface of the central channel of the housing at the axial location of the fan blades.
- a radially inward surface of the annular body of the pinion gear is radially outward of a radially inward surface of the central channel of the housing at an axial location of the pinion gear.
- the fan aspirator may further include a controller electrically coupled to the plurality of motors.
- the controller may be configured to synchronize angular speed of the plurality of motors.
- a gear ratio of the fan aspirator is between 1.25 and 6.
- a gear ratio of the fan aspirator is between 1.5 and 3.
- a gear ratio of the fan aspirator is about 1.67.
- the system may include an inflatable device and a fan aspirator.
- the fan aspirator may be coupled to the inflatable device, and may include a housing, a fan, a pinion gear, and a plurality of motors.
- the housing may define a central channel and may have a central longitudinal axis.
- the fan may be disposed in the central channel and may be configured to rotate about a rotational axis that is substantially parallel to the central longitudinal axis.
- the pinion gear is coupled to the fan and configured to rotate with the fan, with the pinion gear comprising an annular body comprising a gear track.
- the plurality of motors may include a respective plurality of drive gears.
- the plurality of motors are coupled to the housing and are distributed circumferentially around the rotational axis such that each drive gear of the respective plurality of drive gears is mechanically coupled to the gear track of the annular body of the pinion gear, according to various embodiments.
- the system also includes an electrical power source electrically coupled to the motor.
- the system further includes a controller electrically coupled to the plurality of motors and configured to synchronize angular speed of the plurality of motors.
- the plurality of motors may include at least 4 motors, and the gear ratio of the driven pinion gear to the drive gears may be between 1.5 and 3.
- FIG. 1 is a drawing of an aircraft having an exit door and an evacuation system, in accordance with various embodiments
- FIG. 2 is a perspective view of an evacuation system in a partially deployed configuration, in accordance with various embodiments
- FIG. 3 A is a perspective view of an inflatable device in an inflated configuration, in accordance with various embodiments
- FIG. 3 B is a perspective view of another inflatable device in an inflated configuration, in accordance with various embodiments.
- FIG. 4 A is a schematic side view of a fan aspirator coupled to an inflatable device, in accordance with various embodiments
- FIG. 4 B is a side cutaway view of a fan aspirator having a plurality of motors and a respective plurality of drive gears, in accordance with various embodiments.
- FIG. 4 C is a perspective cross-sectional view of a fan aspirator have a plurality of motors and a respective plurality of drive gears, in accordance with various embodiments;
- a fan aspirator and related systems and methods, which utilizes one or more motors to drive a fan of the aspirator to deliver inflation fluid to an inflatable device.
- the fan aspirator includes a plurality of motors and a respective plurality of drive gears configured to drive a pinion gear coupled to a fan disposed within the housing of the fan aspirator.
- the aircraft 100 may include a fuselage 101 having a plurality of exit doors including an exit door 102 .
- the aircraft 100 may include one or more evacuation systems positioned near a corresponding exit door or located anywhere in or on the fuselage 101 .
- the aircraft 100 includes an evacuation system 104 positioned near the exit door 102 , and may include another evacuation system positioned in the fuselage 101 and designed to inflate outside of the fuselage to provide at least one of egress or flotation.
- the evacuation system 104 may be removably coupled to the fuselage 101 .
- the exit door 102 may be opened by a passenger or crew member of the aircraft 100 .
- the evacuation system 104 may deploy in response to the exit door 102 being opened and, in various embodiments, the evacuation system 104 may deploy in response to another action taken by a passenger or crew member such as depression of a button or actuation of a lever.
- the evacuation system 104 includes an inflatable device 200 .
- the evacuation system 104 further includes a fan aspirator 202 , a controller 208 , a pressure sensor 210 , and a power source 212 .
- the inflatable device 200 may be coupled to the fuselage 101 of FIG. 1 , and may be decoupled from the fuselage 101 in response to being fully inflated or to being manually detached in order to allow passengers and/or crew members to safely float away from the aircraft 100 of FIG. 1 .
- the inflatable device 200 may be permanently coupled to the fuselage 101 .
- the inflatable device 200 may function as a slide from the fuselage 101 to a ground surface upon which the aircraft 100 is resting. In various embodiments, the inflatable device 200 may be entirely decoupled from the fuselage 101 at all times, may be removed from a cabin by a passenger or crew member, and may be inflated away from the fuselage.
- the controller 208 may include one or more processors and one or more tangible, non-transitory memories and be capable of implementing logic.
- the processor can be a general purpose processor, a digital signal processor (DSP), an application specific integrated circuit (ASIC), a field programmable gate array (FPGA) or other programmable logic device, discrete gate or transistor logic, discrete hardware components, or any combination thereof.
- the pressure sensor 210 may include any sensor capable of detecting data corresponding to a pressure within the inflatable device 200 (the air within the inflatable device 200 may be referred to as “device air”).
- the controller 208 may be coupled to the fan aspirator 202 and may control the aspirator 202 .
- the controller 208 may further be coupled to the pressure sensor 210 , may determine the pressure within the inflatable device 200 based on the detected pressure data, and may control the fan aspirator 202 based on the determined pressure.
- the power source 212 may include any power storage device such as one or more of a battery (e.g., a lithium polymer battery), a flywheel, or a capacitor.
- the power source 212 may include any power generation device such as a generator.
- the power source 212 may provide electrical energy to the motor(s) of the fan aspirator 202 , the controller 208 , and/or the pressure sensor 210 to facilitate operation of these elements.
- fan aspirator may be coupled to an electrical power line to receive electrical energy.
- the inflatable device 200 is illustrated as fully inflated and separated from the fuselage 101 of FIG. 1 .
- the fan aspirators 202 , the controller 208 , the pressure sensor 210 , and the power source 212 may remain coupled to the inflatable device 200 .
- one or more of these elements of the evacuation system 104 may become detached from the inflatable device 200 before, during, or after inflation.
- the inflatable device 250 may provide egress from an aircraft in various situations.
- the inflatable device 250 may include similar features as the inflatable device 200 of FIG. 3 A .
- the inflatable device 250 may include a fan aspirator 252 .
- the inflatable device 250 may further include a controller 258 , a pressure sensor 260 , and a power source 262 .
- the inflatable device 250 may be coupled to a fuselage of an aircraft, and may be decoupled from the fuselage in response to being fully inflated or to being manually detached in order to allow passengers and/or crew members to safely float away from the aircraft.
- the inflatable device 250 may be permanently coupled to the fuselage.
- the inflatable device 250 may function as a slide from the fuselage to a ground surface upon which the aircraft is resting.
- the fan aspirator 302 generally includes a housing 320 defining a central channel within which a fan is disposed.
- the housing 320 generally extends from an inlet end 321 to an outlet end 322 , according to various embodiments, and thus the fan aspirator may be referred to herein as a ducted fan aspirator.
- the housing 320 may extend from the inlet end 321 that is disposed outside 199 of the inflatable device 200 to the outlet end 322 disposed within an internal volume 201 of the inflatable device 200 .
- the fan aspirator 302 may also include an attachment flange 303 that facilitates connecting the fan aspirator 302 to the inflatable device 200 .
- the fan aspirator 302 includes a pinion gear 344 coupled to the fan and at least one motor 340 with a drive gear 342 .
- the motor(s) 340 may drive the drive gear(s) 342 , and the drive gears(s) 342 are mechanically coupled to the pinion gear 344 to drive rotation of the fan, thereby inducing airflow from the inlet end 321 to the outlet end 322 to cause the inflatable device 200 to inflate.
- the motor(s) may receive electrical energy and convert the electrical energy into mechanical power to drive the fan via the drive gear(s) and the pinion gear.
- the fan aspirator may further include a fan flap located proximate the fan inlet 321 .
- the fan flap may allow airflow to flow downstream (i.e., from the inlet 321 towards the outlet 322 ) and may reduce the likelihood of air flowing upstream (i.e., from the outlet 322 to towards the inlet 321 ).
- the fan 446 may be disposed within the central channel defined by the housing 420 .
- the pinion gear 444 which may comprise an annular body 443 , may be mounted to the fan 446 such that the fan 446 and the pinion gear corotate.
- the rotational axis 403 of the fan 446 may be parallel with (and may be coaxial with) the central longitudinal axis of the housing 420 .
- the fan aspirator 402 includes a plurality of motors 440 with a respective plurality of drive gears 442 .
- the plurality of motors 440 may be coupled and/or mounted to the housing 420 and may be generally distributed circumferentially around the rotational axis 403 of the fan 446 .
- Each of the drive gears 442 may be mechanically coupled to a gear track of the pinion gear 444 , thus collectively driving rotation of the pinion gear 444 and the fan 446 mounted thereto.
- the fan aspirator 402 includes 2 or more motors and respective drive gears. In various embodiments, the fan aspirator includes between 3 and 8 motors and respective drive gears. In various embodiments, the fan aspirator includes 4 motors. In various embodiments, the fan aspirator includes 6 motors.
- the fan 446 may be driven to reach speeds sufficient to drive enough air into the inflatable device. Further, various other benefits may be realized by using a plurality of circumferentially distributed motors, such as efficiency, power consumption, and weight savings over conventional aspirators that rely on a source of compressed gas, according to various embodiments.
- the central channel 425 defined by the housing 420 may have a radial dimension that remains constant along a length of the fan aspirator (e.g., at least along a section of the housing 420 at an axial location of the fan blades 448 ).
- the radial dimension of the central channel 425 may vary along the length of the fan aspirator 402 .
- the fan blades 448 may have a radial span that is less than the radial dimension of the central channel, and thus a radial gap may exist between the outer edge of the fan blades 448 and the radially inward surface of the central channel 425 .
- additional air i.e., induced air
- the gear track of the pinion gear 444 is disposed on a radially outward surface of the annular body 443 of the pinion gear 444 .
- the pinion gear 444 may have an annular structure, thus allowing the air/fluid to flow through the central aperture of the pinion gear.
- the pinion gear 444 may include one or more structural spokes 445 extending radially between the central region of the pinion gear where it connects to the fan and the annular body 443 .
- the respective drive gears 442 may be disposed and distributed around the periphery of the pinion gear.
- the fan aspirator may include a controller electrically coupled to the plurality of motors.
- the controller may be an electronic speed controller configured to synchronize angular speed of the plurality of motors to efficiently drive rotation of the pinion gear and fan.
- a gear ratio of the driven pinion gear relative to the drive gears is between 1.25 and 6. In various embodiments, the gear ratio is between 1.5 and 3. In various embodiments, the gear ratio is about 1.67.
- a radially inward surface of the annular body 443 of the pinion gear 444 may be radially outward of tips of fan blades 448 of the fan such that a radial gap is defined between the tips of the fan blades 448 and the radially inward surface of the annular body 443 .
- a radially inward surface of the central channel 425 of the housing 420 (at least at an axial location of the fan blades 448 ) is radially outward of tips of the fan blades 448 such that a radial gap is defined between the tips of the fan blades 448 and the radially inward surface of the central channel 425 of the housing 420 at this location.
- a radially inward surface of the annular body 443 of the pinion gear 444 is radially outward of a radially inward surface of the central channel 425 of the housing 420 at an axial location of the pinion gear 444 .
- any of the method or process descriptions may be executed in any order and are not necessarily limited to the order presented.
- any reference to singular includes plural embodiments, and any reference to more than one component or step may include a singular embodiment or step.
- Elements and steps in the figures are illustrated for simplicity and clarity and have not necessarily been rendered according to any particular sequence. For example, steps that may be performed concurrently or in different order are illustrated in the figures to help to improve understanding of embodiments of the present disclosure.
- Any reference to attached, fixed, connected or the like may include permanent, removable, temporary, partial, full and/or any other possible attachment option. Additionally, any reference to without contact (or similar phrases) may also include reduced contact or minimal contact. Surface shading lines may be used throughout the figures to denote different parts or areas but not necessarily to denote the same or different materials. In some cases, reference coordinates may be specific to each figure.
- references to “one embodiment”, “an embodiment”, “various embodiments”, etc. indicate that the embodiment described may include a particular feature, structure, or characteristic, but every embodiment may not necessarily include the particular feature, structure, or characteristic. Moreover, such phrases are not necessarily referring to the same embodiment. Further, when a particular feature, structure, or characteristic is described in connection with an embodiment, it is submitted that it is within the knowledge of one skilled in the art to affect such feature, structure, or characteristic in connection with other embodiments whether or not explicitly described. After reading the description, it will be apparent to one skilled in the relevant art(s) how to implement the disclosure in alternative embodiments.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims (20)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP21216584.9A EP4019782A1 (en) | 2020-12-22 | 2021-12-21 | Axial flow fan with a motor radially outside the fan duct and with a gearing between the motor and the impeller |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IN202041055872 | 2020-12-22 | ||
IN202041055872 | 2020-12-22 |
Publications (2)
Publication Number | Publication Date |
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US20220196022A1 US20220196022A1 (en) | 2022-06-23 |
US11592026B2 true US11592026B2 (en) | 2023-02-28 |
Family
ID=82023911
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US17/237,304 Active 2041-05-08 US11592026B2 (en) | 2020-12-22 | 2021-04-22 | Fan aspirator |
Country Status (1)
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US (1) | US11592026B2 (en) |
Citations (19)
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---|---|---|---|---|
US2441446A (en) * | 1944-12-23 | 1948-05-11 | Falk Corp | Fan drive |
US2470794A (en) * | 1943-12-20 | 1949-05-24 | Robert E Snyder | In-line fluid pump |
US3001692A (en) * | 1949-07-26 | 1961-09-26 | Schierl Otto | Multistage compressors |
US3399407A (en) * | 1966-05-03 | 1968-09-03 | Thomas O. Olsen | Cushion for decelerating falling bodies |
US6591873B1 (en) | 2001-11-21 | 2003-07-15 | Air Cruisers Company | Turbo fan aspirator |
US20060172686A1 (en) * | 2005-01-06 | 2006-08-03 | Kuan-Hua Ho | Fan acceleration structure |
US20070134111A1 (en) * | 2005-12-14 | 2007-06-14 | Eybergen William N | Fuel cell compressor system |
US20090004003A1 (en) | 2007-06-29 | 2009-01-01 | Hsiao Li-Hui | Passive fan |
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US20140186197A1 (en) * | 2013-01-02 | 2014-07-03 | Elijah Anim Owusu | Fan assembly having multiple centrifugal fans in mechanical connection with a planetary gear system |
US20140219775A1 (en) * | 2013-02-05 | 2014-08-07 | Samsung Techwin Co., Ltd. | Compression system |
US20150219398A1 (en) * | 2012-11-15 | 2015-08-06 | JVS Associates, Inc. | Contra-rotating axial fan system and transmission for dry and evaporative cooling equipment |
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US9637210B2 (en) | 2014-10-16 | 2017-05-02 | Air Cruisers Company | Electric powered inflation system |
US20180058463A1 (en) * | 2011-10-21 | 2018-03-01 | Prime Datum Development Company, Llc | Load Bearing Direct Drive Fan System With Variable Process Control |
US20180283389A1 (en) * | 2015-09-02 | 2018-10-04 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Compressor |
US20190063444A1 (en) * | 2017-08-22 | 2019-02-28 | Hsiu Hui Yeh | Axleless fan device |
US20190393763A1 (en) * | 2018-06-26 | 2019-12-26 | Pratt & Whitney Canada Corp. | Electric fan |
EP3708488A1 (en) | 2019-03-11 | 2020-09-16 | Subaru Corporation | Rotating device and aircraft |
-
2021
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US2470794A (en) * | 1943-12-20 | 1949-05-24 | Robert E Snyder | In-line fluid pump |
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US3001692A (en) * | 1949-07-26 | 1961-09-26 | Schierl Otto | Multistage compressors |
US3399407A (en) * | 1966-05-03 | 1968-09-03 | Thomas O. Olsen | Cushion for decelerating falling bodies |
US6591873B1 (en) | 2001-11-21 | 2003-07-15 | Air Cruisers Company | Turbo fan aspirator |
US20060172686A1 (en) * | 2005-01-06 | 2006-08-03 | Kuan-Hua Ho | Fan acceleration structure |
US20070134111A1 (en) * | 2005-12-14 | 2007-06-14 | Eybergen William N | Fuel cell compressor system |
US20090004003A1 (en) | 2007-06-29 | 2009-01-01 | Hsiao Li-Hui | Passive fan |
US20090175745A1 (en) * | 2008-01-08 | 2009-07-09 | Denso Corporation | Blower Unit for Vehicle |
US20180058463A1 (en) * | 2011-10-21 | 2018-03-01 | Prime Datum Development Company, Llc | Load Bearing Direct Drive Fan System With Variable Process Control |
US20150219398A1 (en) * | 2012-11-15 | 2015-08-06 | JVS Associates, Inc. | Contra-rotating axial fan system and transmission for dry and evaporative cooling equipment |
US20140186197A1 (en) * | 2013-01-02 | 2014-07-03 | Elijah Anim Owusu | Fan assembly having multiple centrifugal fans in mechanical connection with a planetary gear system |
US20140219775A1 (en) * | 2013-02-05 | 2014-08-07 | Samsung Techwin Co., Ltd. | Compression system |
US20160245293A1 (en) * | 2013-10-03 | 2016-08-25 | Total Sa | Axial ventilation device, premises equipped with such a device |
US9637210B2 (en) | 2014-10-16 | 2017-05-02 | Air Cruisers Company | Electric powered inflation system |
US20180283389A1 (en) * | 2015-09-02 | 2018-10-04 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Compressor |
US20190063444A1 (en) * | 2017-08-22 | 2019-02-28 | Hsiu Hui Yeh | Axleless fan device |
US20190393763A1 (en) * | 2018-06-26 | 2019-12-26 | Pratt & Whitney Canada Corp. | Electric fan |
EP3708488A1 (en) | 2019-03-11 | 2020-09-16 | Subaru Corporation | Rotating device and aircraft |
Non-Patent Citations (1)
Title |
---|
European Patent Office; European Search Report dated May 13, 2022 in Application No. 21216584.9. |
Also Published As
Publication number | Publication date |
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US20220196022A1 (en) | 2022-06-23 |
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